Catalog Search Results


1) STE thrust chamber technology main injector technology program and nozzle advanced development program (ADP): final report

Series
NASA contractor report volume NASA CR-193919
Publisher
United Technologies, Pratt & Whitney
Publication Date
[1993]
Edition
Not Supplied
Language
English

2) Analysis of film cooling in rocket nozzles: final report, contract #NAG8-212, task no. 3

Author
Woodbury, Keith
Series
BER report volume no. 596-37
NASA contractor report volume NASA CR-194674
Publisher
University of Alabama, College of Engineering, Bureau of Engineering Research
Publication Date
[1993]
Edition
Not Supplied
Language
English

3) FNAS/Summer faculty Fellowshop Research Continuation Program task #3 entitled analysis of film cooling in rocket nozzle: semi-annual report, January 17, 1992 - October 17, 1992

Author
Woodbury, Keith
Series
NASA contractor report volume NASA CR-192003
Publisher
[National Aeronautics and Space Administration]
Publication Date
[1992]
Edition
Not Supplied
Language
English

4) Rocket engine nozzle attenuator

Author
Lewis, David A
Series
NASA case volume MFS-28739-1
Publisher
[National Aeronautics and Space Administration]
Publication Date
[1993]
Edition
Not Supplied
Language
English

5) Nozzle fabrication technique: patent application

Series
NASA case volume MSC-21299-1
Publisher
[National Aeronautics and Space Administration]
Publication Date
[1988]
Edition
Not Supplied
Language
English

6) Experimental thrust performance of a high-area-ratio rocket nozzle

Author
Pavli, Albert J
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Publication Date
1987.
Edition
Not Supplied
Language
English

7) Altitude compensating ablative stiffening band for rocket motor nozzles: patent application

Series
NASA case volume MFS-28728-1
Publisher
[National Aeronautics and Space Administration]
Publication Date
[1993]
Edition
Not Supplied
Language
English

8) Performance of an isolated two-dimensional wedge nozzel with fixed cowl and variable wedge centerbody at Mach numbers up to 2.01 / Donald L. Maiden ; Langley Research Center,...

Author
Maiden, Donald L
Series
NASA technical note volume NASA TN D-8218
Publisher
National Aeronautics and Space Administration
Publication Date
1976.
Edition
Not Supplied
Language
English

9) Boundary layer development as a function of chamber pressure in the NASA Lewis 1030:1 area ratio rocket nozzle

Author
Smith, Tamara A
Series
NASA technical memorandum
Publisher
National Aeronautics and Space Administration
Publication Date
[1988]
Edition
Not Supplied
Language
English

10) Convoluted nozzle design for the RL10 derivative IIB engine: final report

Publisher
National Aeronautics and Space Administration, Lewis Research Center
Publication Date
1985.
Edition
Not Supplied
Language
English

11) Comparison of straight and 15 degree vectored nozzles using a six component thrust stand: final technical report, 10/90 - 12/91

Author
Carpenter, Thomas W
Series
NASA contractor report volume NASA CR-193291
Publisher
California Polytechnic State University, m
Publication Date
[1991]
Edition
Not Supplied
Language
English

12) Simulation of preburner sprays: final report

Series
NASA contractor report volume NASA CR-193031
SRA report volume R93-9083-F
Publisher
The Associates
Publication Date
[1993]
Edition
Not Supplied
Language
English

13) Qualification test of the Ross double planetary mixer: final test report

Author
Lueders, K. F
Publisher
Thiokol Corp., Space Operations
Publication Date
[1993]
Edition
Not Supplied
Language
English

14) Final postflight hardware evaluation report, RSRM-29 (STS-54): Appendex D, Nozzle postfire data

Publisher
Thiokol Corp., Space Operations
Publication Date
[1993]
Edition
Not Supplied
Language
English

15) Nuclear thermal rocket nozzle testing and evaluation program

Author
Davidian, Kenneth O
Publisher
[National Aeronautics and Space Administration]
Publication Date
[1993]
Edition
Not Supplied
Language
English

16) Final postflight hardware evaluation report, RSRM-29, STS-54: Appendix C, Nozzle PFORS

Publisher
Thiokol Corp., Space Operations
Publication Date
1993]
Edition
Not Supplied
Language
English

17) Flight motor set 360H005 (STS-28R): Volume V, (Nozzle component)

Author
Smith, D. M
Publisher
Thiokol Corp., Space Operations
Publication Date
[1990]
Edition
Not Supplied
Language
English

18) Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m²(350 psia)

Author
Smith, Tamara A
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Publication Date
1987.
Edition
Not Supplied
Language
English

20) Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds: periodic progress research report for cooperative agreement NCC2-487 for the period Feburary 1,...

Series
NASA contractor report volume NASA CR-191368
Publisher
[National Aeronautics and Space Administration]
Publication Date
[1992]
Edition
Not Supplied
Language
English

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